The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jul. 16, 2019

Filed:

Apr. 22, 2013
Applicant:

Sikorsky Aircraft Corporation, Stratford, CT (US);

Inventors:

Bryan D. Mayrides, Derby, CT (US);

William A. Welsh, North Haven, CT (US);

Steven D. Weiner, Orange, CT (US);

Assignee:

SIKORSKY AIRCRAFT CORPORATION, Stratford, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/10 (2006.01); B64C 27/72 (2006.01); B64C 27/00 (2006.01);
U.S. Cl.
CPC ...
B64C 27/72 (2013.01); B64C 27/001 (2013.01); B64C 27/10 (2013.01); B64C 2027/004 (2013.01); B64C 2027/7216 (2013.01); B64C 2027/7244 (2013.01); Y02T 50/34 (2013.01);
Abstract

A rotary wing aircraft is provided including a dual counter-rotating, coaxial rotor system having an upper rotor system and a lower rotor system rotatable about a common axis. A plurality of blade assemblies is mounted to a portion of either the upper rotor system or the lower rotor system. A plurality of individually controllable actuators is coupled to each of the plurality of blade assemblies. Each of the plurality of actuators is configured to control movement of the coupled blade assembly about a pitch axis. The rotary-wing aircraft additionally includes a sensor system within an airframe. A higher harmonic control (HHC) controller is arranged in communication with the sensor system and the plurality of actuators to individually control the upper rotor system and the lower rotor system to reduce vibration.


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